We provide aerodynamic testing services
The team currently has 27 members.
Among them, 20 hold doctoral degrees.
Our team has developed high-precision, high-resolution numerical simulation methods, created CFD code with independent intellectual property rights, and constructed a high-performance flow field simulation platform. The results have been applied to complex rotor flow and aerodynamic characteristics, aircraft design and flow mechanism research, and aircraft aerodynamic noise mechanisms and noise reduction technologies.
Core Capabilities
NO.1 Large Wind Tunnel Laboratory
Independently developed and built large wind tunnel and impact-load laboratories
NO.2 Wind Tunnel R&D and Testing Capabilities
1. Wind tunnel types: electrically heated wind tunnel, combustion heated wind tunnel, shock wave wind tunnel;
2. Coverage areas: subsonic, transonic, and hypersonic;
3. Research and Application: Fundamental research on fluid dynamics below Mach 8, research on combustion aerodynamics, and ground test verification of model aircraft or engines.
NO.3 Impact Load Simulation and Testing Capabilities
1. Core equipment: Independently developed controllable semi-free piston shock tube;
2. Simulation test types: blast wave, impact load, structural collision;
3. Specific experimental projects: explosion impact test of large ships and armored vehicles, local impact resistance test of building structures, high-speed impact simulation and survival rate verification test of black boxes.
